S

SQUIRE 

IANDER5 

LEGAL 

COUNSEL 

WOR.LDWIDE 

November 1, 2010 

VIA HAND DELIVERY 

Samuel Podberesky, Esq. 

Assistant General Counsel 

for Aviation Enforcement and Proceedings, C-70 

U.S. Department ofTransr xtation 

1200 New Jersey Avenue, ~).E., Room W96-322 

Washington, D.C. 20590 

SQUIRE, SANDERS & DEMPSEY L.L.P. 

Suite 500 

1201 Pennsylvania Avenue, N.W. 

Washington, D.C. 20004 

Office: + 1.202.626.6600 

Fax: + 1.202.626.6780 

Direct Dial: +1.202.626.6840 

cdonley@ssd.com 

Re: Joint Application of TACA International Airlines, S.A., Lineas Aereas Costarricenses 

S.A., Aviateca S.A. and Trans American Airlines d/b/a TACA Peru for Equivalent 

Alternative Determination--Docket DOT -OST -2008-0273 

Dear Mr. Podberesky: 

In accordance with 14 C.F.R. 382.10, TACA International Airlines, S.A. ("TACA"), Lineas Aereas 

Costarricenses S.A. ("LACSA"), Aviateca S.A. ("Aviateca") and Trans American Lines d/b/a T ACA 

Peru ("TACA Peru") (collectively, the "Joint Applicants") hereby apply for an equivalent alternative 

determination with respect to the movable aisle armrest requirement set forth in 14 C.F.R. 382.61. 

Section 382.61 requires that foreign air carriers such as the Joint Applicants ensure that at least fifty 

percent of passenger aisle seats on their aircraft used to provide service to or from the United States have 

movable armrests proportionately in all cabin classes. 

The Joint Applicants currently operate A319, A320 and A321 aircraft to and from the United States, 

and have orders in place for a number of additional such aircraft.' Although the additional aircraft were 

ordered prior to May 13, 2009, they will be delivered after May 13, 2010, thus requiring that they meet 

Section 3 82.61 's armrest requirements in the absence of an equivalent alternative determination. 

1 The Joint Applicants operate these aircraft to and from the United States under interchange agreements 

among them. The aircraft that are the subject of this application are therefore part of a shared t1eet. 

Although the aircraft schematic drawings included with this application are identified as "TACA", the 

aircraft operated by each of the Joint Applicants, including the business class seats (Recaro CL4400), 

the boarding wheelchair (Gerald Simonds Healthcare Ltd. travel wheelchair) and their business class 

seat configurations, are identical. 

CI~t:!~NATi • CLFVEL·\NI> • Cc'l u.~mvs • HousToN • Lus ANc;ELFs • MIA:\.ll ·NEw YnRK • PAlt> AI )'(I • Pl!oFNIX ·SAN f'RA:--:usco • TALLM!ASsH. • T-\Ml'A • Trsor;s CuRNI-.R 

WAsHIN<;ToN DC· WEST P,\J.M BF.ACH i C.-\RAC:IS • Rlt> DE )ANI'IR<l • SA>Hll DnMIN<>O ·SAo P:~mo i BHATISLAVA • BRl'sSJJ.s • Bt'IJAPI·Sr • f'RA;.iKI'\.'In • KYIV 

Lc>~PoN • MclSUlW • !'Rti<;CE • WARs.w; I B~lllN<; • HoN<; KnN<> • SHAN<:HAI • TuKYo I Asso<:IATI'!J f'IRMS: Bct:riA!lEST • Bt:E:--:os AIRFS • Dt:Rl.IN • SANTIAt;o 

\VWV!/.S-"'I..i.t·onl 
SQUIRE, SANDERS & DEMPSEY L.L.P. 

Samuel Podberesky, Esq. 

November 1, 2010 

Page 2 

The business class seats on the Joint Applicants' A319, A320 and A321 aircraft do not have 

movable armrests. However, the configuration of these seats and the pitch in the Joint Applicants' 

business class cabins on their A319, A320 and A321 aircraft make it possible for disabled passengers to 

transfer easily from a boarding chair into the seat without having to be lifted over the aisle armrest. The 

Joint Applicants thus request an equivalent alternative determination with respect to the business class 

cabin seats in their A319, A320 and A321 aircraft. Enclosed with this letter is a DVD demonstrating the 

transfer of passengers from a boarding chair into the business class seats on the Joint Applicants' A321 

aircraft as well as schematic drawings of the aircraft interiors. 

The Joint Applicant's request i:' supported by the Department's findings in drafting Part 332 and its 

decisions in other similar cases. In .ldopting Part 382, the Department recognized that movabk armrests 

might not be necessary where ai:' ;raft and seats are configured in a manner that allow< disabled 

passengers to complete the transfer from boarding wheelchair to seat without lifting the passc.1ger over 

the armrest: 

The Department agrees that, if in a given aircraft, seats and seat 

pitches are configured so as to permit a horizontal transfer of a 

passenger from a boarding wheelchair to the aircraft seat (i.e., a 

transfer that can be accomplished without lifting the passenger 

over the aisle armrest), it would not be necessary to have a 

movable armrest at that location. Consequently, if a canier can 

show, through an equivalent alternative request, that such transfers 

are feasible with a given cabin configuration, the Department 

would grant the request for the canier' s aircraft using that 

configuration. 2 

The schematic drawings and DVD enclosed with this letter demonstrate that the configuration of the 

Joint Applicants' aircraft and the seat pitch in the Joint Applicants' business class cabins permit 

precisely the type of easy transfer contemplated by the Department in adopting Part 382. 

The seat pitches in the Joint Applicants' A319, A3 20 and A3 21 business class cabins are 41. 40 and 

40 inches, respectively. These pitches provide more than ample room for passengers to transfer from the 

boarding wheelchair into a business seat without having to be lifted over the armrest. Exhibit A 

provides a schematic drawing of each of these aircraft. Business class seat pitch is shown in the legend 

on each drawing under the column heading "B/C". 

2 73 Fed. Reg. 27614,27625 (May 13, 2008) 
Samuel Podberesky, Esq. 

November 1, 2010 

Page 3 

SQUIRE, SANDERS & DEMPsEY L.L.P. 

The Joint Ap~licants' request is. con~istent with req~ests from nun:er?us other carriers approved by 

the Department.· In fact, the seat p1tch m TACA's busmess class cabm ts more generous than the seat 

pitch at least one case in which the Department approved an equivalent alternative determination 

involving business cabin armrests. On October 27, 2009, the Department approved a request for 

equivalent alternative determination from Aero vias del Continente Americana S.A. ("A vianca") for 

Avianca's A319 and A320 aircraft. The Joint Applicants' A319 and A320 aircraft provide more space 

in the business cabin aisle and between business cabin seats than do Avianca's aircraft. 

As Exhibit B dem:mstrates, the Joint Applicants' business cabin aisle in its A3l9 and A320 aircraft 

is 24.1 inches wide, compared to Avianca's 23.5 inch-wide aisle. Moreover, the business seat pitch in 

the Joint Applicants' a•rcraft is greater than in Avianca's aircraft. The Joint Applicants offer a seat pitch 

of 41 inches in their /,319 business cabin, compared with a seat pitch of 38 inc·:es in Avianca's A319 

business cabin. The Lint Applicants' A320 aircraft offers a business seat pitch •. f 40 inches, compared 

with a seat pitch of38 ,nches in Avianca's business cabin.4 

Aisle Width 

Seat Pitch 

Aisle Width 

Seat Pitch 

Joint Applicants' 

A3l9 

24.1 

41.0 

Joint Applicants' 

A320 

24.1 

40.0 

Avianca 

A319 

23.5 

38.0 

Avianca 

A320 

23.5 

38.0 

The additional aisle width and seat pitch in the Joint Applicants' aircraft ensure that disabled passengers 

will find it easy to transfer horizontally from the boarding wheelchair to the Joint Applicants' business 

cabin seats, without interference from the seat armrest. 

The enclosed DVD demonstrates the ease with which a transfer can be made from the boarding 

wheelchair to a business seat on the Joint Applicants' aircraft. The DVD shows the unassisted and 

assisted transfer of disabled passengers (male and female) from a boarding wheelchair to first row 

(bulkhead) and last row seats (left and right sides) in the business class cabin of the Joint Applicants' 

3 Equivalent alternative determinations for business class armrests have been approved for Air France, 

Asiana, Avianca, Cathay Pacific, Emirates, Etihad, Japan Airlines and Singapore Airlines. The Joint 

Applicants' request is virtually identical to requests made by these carriers and approved by the 

Department. 

4 A vianca does not operate the A32l aircraft. 
Samuel Podberesky, Esq. 

November 1, 2010 

Page 4 

SQUIRE, SANDERS & DEMPSEY L.L.P. 

A321 aircraft. 5 As the DVD shows, sufficient seat pitch exists to permit passengers 2nd crew to move 

the boarding wheelchair into the seat rows, allowing passengers to make an easy and safe horizontal 

transfer to the business seat w:thout interference from the armrest. The Joint Applicants' submit that the 

configuration of their business cabins, as sho\Vn in the DVD and in the schematic drawings, meets the 

requirements set forth by the Department for a finding of equivalent alternative when it adopted Part 

382. 

The Joint Applicants' will comply with the standard conditions imposed by the Department in other 

cases in which equivalent alterrative determinations for Section 382.61 have been approved, including 

(i) obtaining prior Department a:Jproval for changes in seat configuration or dimension; (ii) ensuring that 

employees and contractors are trained in procedures and the use of all equipment required to complete 

the transfer from the boarding wheelchair to the business cabin seat~ (iii) ensuring anr:ual refresher . . 

training in transferring passeng·rs and retention of training records for three years; and iv) quarterly 

submission to the Department of any complaints received by the Joint Applicants related tJ transfers to 

and from their business class seJ.ts. 

In view of the foregoing, and in accordance with the provisions of 14 C.P.R. 382.10, the Joint 

Applicants' respectfully request the Department's favorable determination that the Joint Applicants' 

may utilize an equivalent alternative to the requirements of 14 C.P.R. 382.61 for the business cabin seats 

in their A319, A320 and A321 aircraft. 

Please contact the undersigned with any questions. 

Very truly yours, 

~:C~CL 

Enclosures 

cc: Docket DOT-OST-2008-0273 (w/o DVD) 

Omar Guerrero, Esq., Oftice of Aviation Enforcement and Proceedings (w/o DVD) 

5 This aircraft employs a seat pitch that is the same as the pitch in the Joint Applicants' A320, and that is 

one inch less than the pitch in their A319 aircraft. The DVD therefore presents a conservative view the 

space that is in fact available to passengers in the Joint Applicant's A319 aircraft. 
EXHIBIT A 
·"' i I I § <Sl . . ~j Ji\ ~ ~ ~ N~ ;o " . " ~ 

;. N i 

~~ E I ~ eg tii!I~S Q~ CD~ ·i:. w ""~ 

l!i ~ ~~~N ~~ s~ ·I· -... CII'ID I" .. >- ~~ ~ Jii I ~ !:!;~ "' ~ &;~'- ""d s: N !' u 

rf ~ 

1¥ ~ u li: ~ m~ s~ L!il •• • ' . ••:m ;! ii L li ... :~ ~ ,; i ~~= • ~ J i!~ • ~- i! • l f. ~:..; ! =~! ~i· , se~.o:-: ~ ~~ ~!=i= iii~ .. = ' .. .. ::!i § ~ ;! ~ .. i . Ul !'~-

U-•• . ~.~ " "' . ~~. ~ ~!ii ~ ~ .. ~ .. h~: i5lll ~~St ""l 1--

£ ~S""'i . ~~~ ~ ffi

0i ........ ;o :!l" ill~ H .. :!!: I ~ ! ~: d" a ~;i!~ 'i -z::; ffi '!i ~ .. ~ ~~~ gH~i :;:L§ ·~: ~ .. .. 

~ , ... ' ... j ~ .i. ~ I ii ~ 

i • ;;; !: ~ 5 f'! f''' 5' 8' " ~ 

1-

!J r; lj 

~ ' 

i I ........... l 
T OR~G NO : 22901 Page : 1 2/9/2808 15:07:21 

C12 Cl< Cl6 C!B C20 C21 C23 C2+ C25 C26 C27 C2B C29 C3B C3+ C35 C36 C37 C3B C39 C+B C+1 C+2 C+3 CH C+S C+G C+l/51 C52 C53 C5+ C55 C56 C57 CSB C59 C6B 

"' .. ... 

N 

J&.s• I 

FRONT SfLJO DIMENSIONS 

<AI !f'"BT"I (Ct IWHCE)\ SAP 

FtC 

ere 

VIC lC?j•( 1S.0"f27.2• 

Y/C2 

FtC ei! BIC J+.S'\19.0'!29.8' 

b Y/C 13.8• 1!1.0' 2ll.3' o: 'Y/C2 

1 1 { \5.7' 

11.1-" 

" ... 

"' "' 

B S' 

2 3 

~B 

I F3-B',l 2.•·u.e•=a2.a• ~ -tJ .e~ 

" " " "? "' "' 

"' N .. N Ul "' "' "' .. 

.I 

"? 

L'l 

ill 

m 

.-

.. 

"' "' 

.I 

... 

"' 

" Ill 

OF 2.5" 

VIDEO GARAGE. SEAT DIMENSION CAl= 2.7• 

PROVISIONS FOR ~HEELCHA: 

~ 

t 

~~~~ 5 6 7 8 9 §~~§§§§§§~ 10 11 12 13 !+ 15 16 17 18 IE 

§~~[] §8§§8§§§§8[ 1.•31.a'=t2-t.e• 1J.e• 5. *33.8"=165.8' r .... 32.e•=z2t.e• 

*1 

~ ABREAST CONSTANT SECTION 6 ABREAS 

ALL SEATS ARE BACKREST VIDEO EXCEPT RO~ 3. 

*1 : VIDEO ARM ON SEATS 4A. B. C. D. E. F. 

67.•• 24,1• 57.e• ~ 

J. 
T ORWG NO : 22SI:?Jil Page 2 

; C57 C56 C55 CGB C6l C62 CGJ CG• C65 C66 C67 C66 CGS C70 

I I 

"' "' .. ;;; ~ .. ~ " " ., 

>= 2.7" .. .. ffi 

~ .,; 

lONS FOR WHEELCHAIR INSTALL.ATION " 

@j 

36.6' 

Typo en 

STRETCHER LOADING CAPABILITY 

~~~ 

~ ~ ;. 

U> ~ "' "' it 01 

"' ~ ~ ~ ~ 

[§I] STRETCHER LOCATION 

[f@ MEDICAL OUTLET 

6 ABREAST CONSTANT SECTION [li] STANDARD LITERATURE POCKET 

[ili] LCD SCREEN 

+~ [8] HANDICAPPED FACILITIES 

[8] FULL HEIGHT 

ffiQI BELOW OVERHEAD STOWAGE COMPARTMENT 

IBID NO BREAK OVER 

[]] NARROW SEAT 

!hiD Ll M !TED RECLINE 6\.2• h7.9•! &1.~· I G IN ARMREST TABLE 

[ill NON TEXTILE FLOOR 

l. 

~;;,; . ..:::;11)6 1-. 

Airbus 

REV I DESCRIPTION 

- FllO CABIN PART MOVED 2' BACK~ARD. 

-AFT CABIN PART MOVED I' FORWARD. 

Dl I - SEAT DIMENSION REVISED. 

- STRETCHER ON ROW 18 • 

- INFLATABLE SEAT BELT ON RO~ I. 

E I I - NOTES ADDEO. 

- INFLATABLE SEAT BELT REMOVED. 

E2 I - H REMOVED ON ROWS 2. 3. 

- LIH!TEO RECLINE OM ROll B CHANGED TO 2,5' 

REMARKS : 

CABIN INFORMATION F/C I B/C 

PASSENGER SEATS : - PITCH - ABREAST 

GALLEY : - GALLEY VOLUME CCUFTl 

-·GALLEY VOLUME CCUFTl/PASS 

- TROLLEY OTY 

0 

e 

0 

0,0 

Cl - l- ~c::T~ r1TY f-.----c . - -------- - LAVATORIES : 0 - PASS / LAVATORIES 0.0 

COAT CLOSET : 0 

-COAT ROO CINCH/ PASSl 0.e· 

STOWAGE : 0 

ATTENDANT SEATS : 

CREW REST SEATS : 

I 12 

"1" 

4 

I 

92 

7.7 

"1.0 

1 

1 

12.0 

0 

0.0" 

2 

DATE 

161512008 

1117/2008 

2/9/2008 

Y/C Y/C2 TOTAL 

108 0 32"/33" 120 

6 

2 

I 

185 0 277 

1.7 0 

7.0 0.0 11.0 

~ 0 3 

2 0 3 5"1.0 0.0 

0 0 0 e.e· 0.0" 

0 0 2 

&TRtroARll itt£GH CDitfORT 

6 0 6 

0 

IHE til II lllDUl AijD_ft_r R£yiSfofTJ) If Jilll Dill 1£ EflCIItCifil.itjiiRitiUil AGR!Eft£~1 OF THE RESP!tllll m•s I SCI'S. 

!ATIUI JS·SUBJICI 10 CHiiG£ aFTER FliRt &Ill£! RIDS£!! D£51&1 liD D!flilflil Uf YID£0 i!SIALIRTIDI. SIDift&IS, DDI HOUSES ETC. 

THIS DIAMI 6 IS IH£ PiBPIR!l QF AIRBUS - Ill illifS llllil£1 

DATE: 21912008 A319-100 CABIN CONFIG FOR: TAl 

ORAIIN : Tl SON 

CERTIF : FAA TACA 

SPEC;6.0 ACG:2.1 

RFC NO : SCALE 1/50-~ OR~G NO: 319-25.22801 !sHEET:011 REV: £ I ITE: 2 
I

n 

?: i! 

~m "•!Oil~&:!lllsz 

~ ~~ID ,_ ... ~ 

j 

• 

1-

·~ 
rtJ 

~ 

Cl2 C!< 

I 

.. '" 

"' "' 

OFU-lG NO : 227Sa T Page : t 29/8/2008 H: t 1 :28 

... ,--,~~~~-~~~~-~~~~~-~~~~-~~~--~~~--~~~---~~-------.----=: 

ClS CtB C20 C21 C23 C2i C25 C26 C27 C28 C29 C3B C:U C32 C33 C31 C35 C36 C37 C38 C35 C10 C. .. l C-1-2 C-1-3 C"t1 C1-5 C1-6 C.17 C"IB C19 CSB CSl C52 C53 CS-+ C55 C56 cs; 

"' '"l(J 

FOOTWEEL RECESS 

_23.a•l 2.•1e.e•~ea.e• 11.e~ 

*1 

.I .I .. .. ~ ~ 

ROW 9 LH/RH SPECIAL UPRIGHT POSITION 1.5'/23' 

ROW 10 LH/RH SPECIAL UPRIGHT POSITION 1.5"/22" 

STD Y/C IAT SEAT WITHOUT VIDEO GARAGE SEAT DIMENSION <A 

~~~~~ ~ ~~~~~~~~~~~f Gtlt1Jt1Jt1JIJ tj dGDt1Jt1JGtlt1J GOGDGDGDGtl1 5 6 7 B 9 10 11 12 13 1~ 15 16 17 IB IS 20 21 

§EB§BB § §§88§8888881 

s.•aLe•;:tss.e• 39.8' I 39.8" 1.•32.6"='22-4.0' 8.•31.0 

*1 

FRONT STUD O!MENSJONS ~ ABREAST CONSTANT SECTION 6 ABREAST CC 

.---.. -., <Ul ICl ALL SEATS ARE BACKREST VIDEO EXCEPT ROW 10, ROW 3. I 101 tEl SRI' 

A A FJC *1 : VIDEO ARM ON SEATS 4A, B. c. o. E, F. I 

! BIC + J Y/1: 2.7• 19.0' 27 .2~ ... 15.7• AND llA, B, c. 0, E. F. i Y/c;! 

t 

F/C 

BIC ... a• ts.a• 28.8• 1• ts.a· =s1.e• 24.,. 57 ••• 

Y/C2 

YIC 3.8" 19~0· 28.3" 6' 15.7~ 

~ ..L 
r 

T DRWG NO : 22768 Page : 2 2S.t8.1:2BB6 1-+: 11 :20 

-~~-~-~~·~--~-

C53 C&t CSS tSE. C57 C58 CSB CG0 C6l CS2 C63 CS-4 CBS. CS6 C67 C68 CEiS C79 

m 

~ ~ 

.. 

N 

i" /23" 

.5"122" 

PRO¥ISJONS FOR WHEELCHAIR INS 'ALLATION 

cAT DIMENSION !Al=2.7" 

e.•lt .e••:i!1&,e~ .l ~-·· !.....\..... l 

6 ABREAST CONSTANT SECTION 

1- ••. .- l''·~~ 

.L 

STRETCHER LOADING CAPABILITY 

!§II STRETCHER LOCATION 

@ MEDICAL OUTLET 

!h§j STANDARD LITERATURE POCKET 

I@ LCD SCREEN 

[BJ HANDICAPPED FACILITIES 

[Bj FULL HEIGHT 

@jJ BELOW OVERHEAD STOWAGE COMPARTMENT 

~ NO RECLINE AND NO BREAK OVER 

IE@ NO RECLINE 

[!jill NO BREAK OVER 

[ill NARROW SEAT 

[J IN ARMREST TABLE 

~ NON TEXTILE FLOOR 

Airbus REV DESCRIPTION OAT£ 

- HALL MOUNTED LCD + SEAT DIMENSIONS REVISED • 

01 - INFLATABLE SEAT BELT A00£0. 

- REPITCH OF BIC. 16/5/2888 

- STRETCHER ON ROW 23. 

El - NOTES ADDEO. 1117/2008 

£2 - INFLATABLE SEAT BELT REMOVED. 

- REPITCH OF ROW 16. 17 AND 26. 29/B/2808 

REMARKS 

CABIN INFORMATION F/C 8/C Y /C l Y /C2 l TOTAL 

PASSENGER SEATS : 0 12 138 ·I 0 - PITCH +B" 31" /32" 1150 - ABREAST 4 6 

GALLEY : 2 ·::-.:.... ~ t""v VOU.!MF C cus=-T) 0 92 !.85 0 277 

- GALLEY VOLUME CCUFTl/PASS 1'1 7.7 1.3 1'1 

- TROLLEY OTY 1'1.0 +.0 7.0 0.0 1!.0 

- WASTE OTY 0 t 2 0 3 

LAVATORIES : 0 1 2 0 3 - PASS / LAVATORIES 1'1.0 12.1'1 69.1'1 1'1.0 

COAT CLOSET : 0 0 0 0 0 -COAT ROO CINCH/ PASS> a.a• 0.1'1" 1'1.1'1" 1'1.0" 

STOJ..IAGE : 0 2 0 0 2 

ATTENDANT SEATS : STAAOAIIO IGH COt1fllfH 

6 0 6 

CREJ..l REST SEATS : 0 

Iii Cllff]:IIOII Alii ilrl[jTSJDliD II I Ill illT II lf!tllll Ifill UililltlllliiiHHiijfOfTMl IHP£Uij(if£CI/ 1[1'5. 

llliUI IS SUIJ£tl li ti!-S[ Ifill Fll!liAll[IIID SUI lfilll liD DHI\IIIM IF IIDlD IUIBilliJII, UDMIII!. Ill iiUS£5 !IC. 

IllS DiRMIIi II IH[ PUPlill If liliUS • Ill il;ill I[S[Il!D 

OATE: 2St812888 I A320-200 CABIN CONFIG FOR: TAI 

DRAWN : TISON 

CERTIF : FAA TACA 

SPEC:7.8 RCG:2.8 

RFC NO : SCALE 11581 ORWG NO: 320-25.22768 IT£: 2 
! "·-· ---c 11...4..,"77'77: 

: .w- J ~ .~-. .....,....,.....,. I 

~~-­

-~-.. -.... a 

: ~ I ; ! 

! i I 

l 

a 

! 

; 

! 

! 

I 

j--. 

... 

I 

I 

I 

I 

i 

1---

i 

I 

I 

I 

! , __ _ 

. "11 i \ I --"···" 

!I ~ . I -·"··-- : 
T OR~G NO : 22"l-B3 Page : 1 1617/2008 10:59:56 

C12 CH C16 CIS C20 C21 C23 C24 C25 C26 C27 C28 C29 C39 C31 C32 C33 C34 C35 C35.2 00 "' ·w Ill C36 C37 C38 C39 C 

I 

., 

., 

"' "' 

36.6' 

.. "' 

~ 

"' 

FRONT STUD DIMENSIONS 

__ <A.>_j 18) I IC) J<O>J<E>J SRP 

FtC 

BIC 

Y/C !2.7'1 19.0' !27 .2•! !••\15.7' Y/C2 

F.iC 

9/C 4.9' 

~ 

1\l 

a 

il.i' 

I 

;. 

,.; 

"' u 

"' "' ., 

RECESS 

*?. 

...... 3t.8'=12of.8' 

*4 

ALL SEATS ARE BACKREST VIDEO EXCEPT *1. *2, *3. 

*1 : NO BACKREST VIDEO IN 8/C SEAT ROW. 

~ ~ 

<li 

.- " "' "' ,.; "' "' "' u "' u "' u "' u "' u 

*6 *5 *5 

*6 *5 *5 

*2; NO BACKREST VIDEO IN STO Y/C SEAT CC=26.2"l, BACKREST LINIG-UP. 

*3: SEAT 21A,21F NO BACKREST VIDEO. <27.2" FROM CUSHION TO BACKREST!. 

*4 : SEATS 8A.8B I,C ~'.REP:~n"':;~ 1 fMTTFn RECLH~E l". 

*5 : VIDEO ARM ON SEATS 4A, B, C, D. E. F, 98, C. D. E. 

AND 10A, F. AND 23A, B. C. 0, E. F. 

*6 : SPECIAL UPRIGHT POSITION 1.5"/23". 

"' "' u 

J... 

J 

"' 

.-

~ 

ta. •:.H .a• 

NO BACKTABL 

~ 
T 

"' .. "' "' ~ 

"' "' "' "' on 

"' '" "' ~ "' C) u u tJ 

6 *5 •·5 

*6 *5 *5 

:KREST L!N!G·-UP. 

ION TO BACKRESTl. 

E, 

---------·· 

., 

"' "' u 

l_ 

T ORWG NO : 22403 Poge : 2 16/7/2008 lB: 59:56 

~~·~-~~·~~~~~~-~~~~~~-~~~~~~~-~~~~~~-~~~~~~-~~-

C36 C37 C39 C3S C~U C-t I C~2 C<3 CH CiS C<G C<7 N C17 .3 .. J .I " 6 ~ " .. " "' u u 

~ i 

*2 

"' c<e C<S csa est C52 CS3 cs< C55 C56 C57 cse C5S csa C61 C62 C63 

..: 

... 

u 

WHEELCHAIR PROVISION 

*5 

~HHS1EflBE]H ~tiltil~~~~~~til~ 24 25 26 27 28 29 30 31 

~BEBEBEBEB EB BEE BEl 

C6i 

I 

.. 

... 

:'.; 

*2 

C65 

i 

.. " 

~ 

C66 C67 C68 

io 

"' .;

U1 

U1 

13.•at.a•_-•a3.e' I / 1 ~ •a. a• L 31.0' ~ \ tB.•32.B'=32B.B' ~ 2s.a• ~ 36.6' J i2.i' 1 rr , ' 

NO BACKTABLE, NO COAT HOOK 

*3 *5 

~ ABREAST CONSTANT SECTION 6 ABREAST CONSTANT SECTION 

r; \\ I 

_! I 

_j -t- b 6 

y~ \ 

IT\\ !rrn~T~~rnl I 

-tI I 

v.e• 2"1.1• ~7 .e~ 61.2. l7.S' 61.2" -

l_ 

CGS C7B 

I 

:;., 

<0 

~ "' 
T ORI-46 "10 ! 22 ... 03 Page ~ 3 16/7/2008 10:59:56 

---- ~ 

:&2 C63 CG• C65 C66 C67 C68 C6S Cl8 Airbus ~ 

~ ., ! REV DESCRIPTION DATE ., - ~ 

~ ~ .. II - NB ON RO~ 8 + STHETCHER ON ROW 31RH + ACG: 2.1 29/-112008 "' lfl ·--·. - Jl - SEAT DIMENSIONS REv ib£0. ... ·· 151512008 

"' ., Kl - NOTES AND DOGHOUSE 08 AOOEO. 161712008 "' "' - SPECIAL UPRIGHT POSITION 23' AND RB ON ROW 9. 10 "' ill ~ ~ *2 

"' 1pe c n 

REMARKS : 

! 

CABIN INFORMATION F/C B/C Y/C Y/C2 TOTAL 

PASSENGER SEATS : 0 12 182 0 - PITCH 40" 31"/32" 194 - ABREAST 4 6 

GALLEY : 2 

~STRETCHER LOADING CAPABILITY 

- GALLEY VOLUME lCUFTl 0 92 185 0 277 

- GALLEY VOLUME (CUFTl/PASS 0 7.7 1.0 0 - TROLLEY QTY 0.0 4.0 7.0 0.0 11 .0 

- I-IASTE QTY 0 1 2 0 3 

~'" 

:rw 

LAVATORIES : 0 1 2 0 3 - PASS / LAVATORIES 0.0 12.0 S1.0 0.0 

COAT CLOSET : 0 0 0 0 0 -COAT ROO CINCH/ PASSl 0.0" 0.0" 0.0" 0.0" 

®] STRETCHER LOCATION STOWAGE 0 2 0 0 2 EQl : MEDICAL OUTLET - .. 

!bill ATTENDANT SEATS : STRNOAAD HU:iH COI1FDRT 

STANDARD LITERATURE POCKET 6 

[@) PERSONAL BULKHEAD VIDEO LCD 6 0 

0 HANDICAPPED FACILITIES CREW REST SEATS : 0 

[8] FULL HEIGHT !HI tAll~ lUQUI A~D A~l lEVI SID~ 10 II Nlll Oijl! IE EHCIIIE. BFIEI COijliAtiUAl BGi!EKEII Of IHE I!SP!tii!E lft"S I Sti•S. 

@ID B IN. DOGHOUSE WITH DOOR liTDUf IS SUBJ!tl 10 CHA-SE lfi!R fliAl Gill[! 1-1 S£81 OESI&i liD OEfliiiiD- Of VIDEO liSIIlllliDi. SIDRAUS. DOG HOUSES fit. 

!HIS ORIN!~& IS 1HE PiOPEII! Of lliBUS • All il&HIS i[S[II[D 

[@] BELOW OVERHEAD STOWAGE COMPARTMENT OATE : 16/712008 A321-200 CABIN CONFIG FOR: TAI 

0ID NO RECLINE AND NO BREAK OVER 

II@ NO RECLINE ORA~N : CLEVE 

[@] NO BREAK OVER CERT!F : FAA TACA 

QTI NARROW SEAT 

0 IN ARMREST TABLE SPEC:i.3 ACG:2.1 

!ill) NON TEXTILE FLOOR RFC NO : SCALE 1150 I ORIIG NO: 321-25. 22~03 I SHEET: 011 REv: K J IT E: I 

l. 
EXHIBIT B 
z 

0 

V1 -

~ 

<( 

c.. 

~ 

0 

u 

0' 

~ 

M 

<( 
AVIANCA 

WEBER 8/C C7070> 

4 ABREAST CONSTANT SECTION 

57.01 67.01 

TACA 

RECARO 4400 

4 ABREAST CONSTANT SECTION 

57.0" 57.0" 
(A) 

(c) 

TACA -7 

BC: RECARO 4400 

YC: RECARO 3510 

! 

0 

.... 

Ill 

0 

co 

(A) 

F/C 

8/C 

Y/C 2.7" 

Y/C2 

4-J F/C 

AVIANCA -7 

BC: WEBER 7070 

YC: WEBER 5750 

Ul 

GIG! 

~- 8/C 4.8" 

Lo 

0 4-J 0 Y/C 3.8" 

c 

- Y/C2 --·~----· .-

~ <A> 

F/C 

u 8/C -

4ft 

~ Y/C 3.2" 

Y/C2 

4-J F/C 

Ill 

.... h- 8/C 3.0" 

h8 w Y/C 6.0" 

c 

.... Y/C2 ;..__ 

( 8) (c) { 0) <E> SRP 

19.0" 27.2" 4" 15.7" 

19.0" 29.8" 7" 19.9" 

19.0" 28.3" 4" 15.7" 

<B> (c) <D> <E> SRP 

18.0" 25.4" 18.2" 

23.0" 27.8" 18.81f 

21.0" 28.2" 21.0" 
. . . ~ Ci) (SJ 

(0 (\) 1\) 

~- ().) ,.. (() (\J (\) (\) M 

~r~1 Tuoa c 

. . <0 ro m lJ) 

... (I) rom "<" ..... (\J(\1 (\j (\j ('I) (l) 

;{>DDTWEEL RECESS 

ITEM 2: 131 in 

.. 7 I .. 

I "/'"'" ~ 

Curtain as soft divider: 

allows to waive r=35in 

head-strike rule to hard 

9 10 

11 • ~' I I -+ • ~ 31 • i:P ,.12'1. 3 • 

N 

If) 

(f) 

~ 

(') 

... 

. 

CSi 

1£) 

ln 

..... 

'f' 

• CSI 

Ol 

m 

m 

lil 

N 

... 

t() 

Pitch between exit 

mws seats 
. 

1$) 

U) 

,... 

... 

(\1 

~ . 

l) 

J) 

.... 

... 

:\1 

:lG. 6" 

36.6" 

. 

1$) 

(\1 

-

m 

(\1 

+ 

• (Sl 

lO 

w ' 

...... 

N 

31 ..... 

~ . (S)(Sl 

(Sj ..... 

.. 

WI'-. 

{T)(f) -- ·~ 5 ~ . 5 

10\J) ~ m . .. .. 

. 

1$) 

. ~ 

. . . ~ classes = 56 in~ ..-to tn 

!1)!1) ...... M '(-- ot--t- ..... 

Partition: r=35in rule from seat to 

monument applies, thea·efore, more 

space is required from monument to 

first.seat row 

Pitch between exit rows 4 

in less than TAI's to allow coi . 

(\1 

for more pitch in YC fwd CSl 'Of" 

to tD 
z 

0 

l/l -

et:: 

<( 

a_ 

~ 

0 

u 

0 

N 

M 

<( 
AVIANCA 

WEBER 7070 

4 ABREAST CONSTANT SECTION 

57.0fl 57.011 

TACA 

RECARO 4400 

4 ABREAST CONSTANT SECTION 

57.0" 24.1" 57.0" 
<A) 

(c) 

TACA~ 

BC: RECARO 4400 

YC: RECARO 3510 

AVIANCA ~ 

BC: WEBER 7070 

VC: WEBER 5600 

u 

-II) 

0 

m 

.t-1 

II) 

Q) OJ t.._ 

ED 

L 0 

C.,.; 

c 

.... 

u 

... 

ta 

0 

CD 

>J 

loll 

.... i-15§ 

c 

-

(A) ( B > 

F/C 

8/C 

Y/C 2.7" 19.0" 

Y/C2~ 

F/C 

8/C 4.8" 19.0" 

Y/C 3.8rr 19.0" 

Y/C2 

(A) (8) 

F/C 

B/C 

Y/C 1.9" 18.0" 

Y/C2 

F/C 

B/C · \r,;= ~ ... -:.... ~" · . .MM.'I...i ?~ .. ... 0" 

Y /C 1 • 9" 18 • 0" 

Y/C2 

(c) (0) <E) SRP 

27.2" 4" 15.7" 

29.8" 7" 19.9" 

28.3" 4" 15.7" 

CC> (0) CE> SRP 

2-4.4" 17 .. 7" 

27.8l'l 18.8" 

24.4" 17.7" 

-
t ..... t:·:· 1 If 

,::;· ( ::; f= :::. f1 

Curtain as soft divider: 

allows to waive r=35in ; 

head-strike rule to hard 

I M : !===·· ;,J, [ill I] ~ ' II t7nH1tfj:- ~~===~ 

STD y, 

11! 

l&.s• I ;u• I I».B•II 2.•10.0'•00.2' II it.B' I I 5.•>1.0'•155.2' ~ft~ l!!.Z' 

m ~ I\IIN (";) ro ro ro ro 

Ill U) IS) 6.'1 ~ 6.'1 ('>) <>I Q.l ~ . . .. ·~ . \ " .. ~ 

~· w ~ o) N . ~ !') Pitch between exit ai ...: ~ .... " (\,( ti) '' (!') " (l,f U) .... 

1\1 N (') (1) T "' rows seats w w " 
. . IS) IS) .... 

lD N lSI 

a by Bassi nets 

. . . "f" - lD .... ll) - N (\1 (") 

36.6~ . 3-4.9 1 

ITEM 2: 128 in 

36.6• 2.*38.0•=76.0• l 

"' • .. co IS) IS) 0'1 l.O IS) 

- (IJ U)t.,. (") 0'1 ISlN m "f" " ~ 

~ - I[)Ul Ul (\1 (\1 (")(') ... ...... ... 

Partition: r=35in rule from seat to 

monument applies, therefore, more 

space is required from monument to 

fi 

Ill 

11 

5. •32.0'=160.0' !l~·~u 37.0' 

~ IS) " .lSI " " IS) IS) IS) IS) 

Pitch between exit rows m " .... N l.O lSI 

is less than TAI's to allow w w " 

for more pitch in YC fwd 

m 

z 

~